Classifications

• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
  • G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
  • G01F1/76—Devices for measuring mass flow of a fluid or a fluent solid material
  • G01F1/86—Indirect mass flowmeters, e.g. measuring volume flow and density, temperature or pressure
  • G01F1/90—Indirect mass flowmeters, e.g. measuring volume flow and density, temperature or pressure with positive-displacement meter or turbine meter to determine the volume flow
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
  • G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
  • G01F1/05—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects
  • G01F1/10—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects using rotating vanes with axial admission
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
  • G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
  • G01F1/05—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects
  • G01F1/10—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects using rotating vanes with axial admission
  • G01F1/12—Adjusting, correcting, or compensating means therefor
  • G01F1/125—Adjusting, correcting, or compensating means therefor with electric, electro-mechanical or electronic means

Definitions

• This invention relates generally to the field of turbine flow meters, and, more particularly, to a method and apparatus for using volumetric turbine flow meters to measure mass flow through the meter.
• duct refers to any tube, conduit, pipe, or the like through which a fluid flows.
• One major market for such meters is the aircraft industry which wants to have accurate mass flow rates for its aircraft. This allows an aircraft to load the imnimum weight of fuel for given flight including an appropriate safety margin. If an aircraft loads more than that minimum weight, it is essentially burning excess fuel to transport that excess weight to its destination. Thus, there is an incentive to provide accurate mass flow numbers for the aircraft industry as well as other applications.
• One method is to use two different flow meters to measure mass flow.
• a volumetric flow meter insensitive to density is used in combination with a density sensitive meter which is used to determine the density of the fluid.
• a density sensitive meter which is used to determine the density of the fluid.
• Turbine meters are often used as the volumetric flow meter, but such meters are very sensitive to the viscosity, temperature and Reynolds number of the fluid being measured.
• Figure 1 shows the classical correlation curve of a standard turbine meter. The illustrated curve graphs the meter frequency divided by the fluid kinematic viscosity is a function of the meter frequency divided by the volumetric flow rate. If a turbine meter is operated at varying temperatures thereby varying the viscosity, the flow rate cannot be determined without knowing that viscosity.
• volumetric flow meters can be used in a similar fashion but all suffer from the same deficiency as the turbine flow meter.
• many other types of flow meters do not have sufficient accuracy to be competitive with the better mass measuring devices.
• density measurements there are a number of meter used including differential pressure meters such as orifice plates and target meters which are all sensitive to temperature, viscosity and Reynolds number.
• flow sensitivity is a function of the square root of the differential pressure of force signals generated by the meters.
• most current metering systems employ direct mass flow measuring meters for such measurements.
• a Coriolis meter which tend to be quite expensive.
• Another direct flow meter employs two turbine elements in tandem wherein one turbine element employs straight turbine blades while the second meter uses a more conventional curved design.
• the two elements are coupled using a torsional spring.
• the torque reaction causes a phase shift between the two blades.
• the phase shift is a function of the mass flow rate as long as the rotational speed of the two elements is constant.
• Several designs are used to maintain the constant rotational speed, including a synchronous motor and a centrifugally loaded vane set.
• Fig. 1 is a graph showing a typical universal viscosity curve for a turbine meter
• Fig. 2 shows a typical Strouhal Number versus Roshko Number correlation plot for a dual rotor turbine meter
• Fig. 3 shows a graph of a dual rotor turbine meter frequency ratio as a function of the o Roshko number for an untrimmed rotor
• Fig. 4 plots a typical fluid viscosity versus temperature curve
• Fig. 5 plots the Strouhal number using a frequency ratio, each as a function of Roshko Number for a dual rotor meter that has not been trimmed
• Fig. 6 plots the dual rotor turbine meter frequency ratio as a function of the Roshko number for a meter that has been adjusted to a non-linear relationship;
• Fig. 7 plots Strouhal number using frequency ratio for the adjusted non-linear meter, each as a function of the Roshko Number for a dual rotor meter that has been trimmed to be non-linear;
• Fig. 8 is a graph demonstrating fluid density versus temperature with a normal upper and a normal lower limit
• Fig. 9 shows the technique for trimming a rotor
• Fig. 10 shows the assembly of a mass flow meter.
• the present invention employs a dual rotor turbine meter 10 described in U.S. Patent No. 5,689,071 entitled "Wide Range, High Accuracy Flow Meter” which issued on November 18, 1997 to Ruffner and Olivier (the present applicant) which is herein incorporated by reference and is illustrated in Fig. 10.
• U.S. Patent No. 5,689,071 describes the operation of two counter rotating hydraulicalfy coupled rotors 18, 20 in a single housing. While operating in many respects like a conventional turbine meter, the patented meter has superior properties in others. Specifically, the operating range is greatly extended. Further, by monitoring the output frequency of both rotors 18, 20, self-diagnostics can be performed. As described in U.S. Patent No. 5,689, 071, the Roshko Number and the Strouhal
• the Roshko numbers for each rotor are:
• v kinematic viscosity of the fluid at T op
• T op operating temperature from a temperature gauge 16 of the meter
• T jgf reference temperature of the meter (may be any convenient temperature).
• the Combined Roshko number Ro c is defined as:
• the Combined Strouhal number St c is defined as follows:
• centistoke viscosity 16 and rotor 2 data taken at 1 centistoke viscosity 19 forms a
• the Roshko number is dete ⁇ ined by measuring the frequency of a rotor, dete ⁇ nining the kinematic viscosity as described in detail below, measuring the operating temperature and then solving the above equation.
• FIG. 2 A typical Strouhal number versus Roshko number curve for a two rotor system is shown in Fig. 2 along with a combined Strouhal number (St c ) curve. Note that the curves are non-linear with rotor 1 tending to have a declining Strouhal number (St,) as its Roshko number (R ⁇ j) decreases and rotor 2 tending to have an increasing Strouhal number (Stj) as its Roshko number (Ro 2 ) increases over most of its range. At lower values, both curves decline. A review shows that there is little or no Roshko number range where either rotor is very linear. However, the combined (average) Strouhal number (St c ) is much more linear, at least at the higher Roshko numbers.
• the Roshko number it is not possible to directly determine the Roshko number without knowing both the rotor frequencies (f_ and f 2 ) and the operating kinematic viscosity (v) of the fluid.
• the rotor frequencies (f, and f j ) are measured and usually the kinematic viscosity (v) of the fluid is predetermined as a function of operating temperature (T op ).
• T op operating temperature
• the kinematic viscosity (v) is also known.
• the fluid is water, the viscosity versus temperature curve is reliably obtainable from textbooks and other sources. The viscosity values of pure water do not vary much, if at all, from the values in published temperature/viscosity charts.
• the viscosity versus temperature relationship for other fluids should be empirically determined for each batch of fluid used.
• the viscosity/temperature relationship can vary greatly from one batch to another depending upon such factors as the origin, manufacturer and constituents of each batch. It is quite common for the viscosity of a given fluid to vary as much as ⁇ 10% from one batch to another at a constant temperature as shown graphically in Fig. 4 which plots textbook data 25 with upper and lower limits 24. Since the Strouhal number versus Roshko number curve in non-linear, such 10% changes can yield a significant change in the Strouhal number for a given output frequency (f).
• the frequency ratio (f 2 /f x ) is considered as a function of the combined Roshko number (averaged number) as shown in Fig. 3, it is shown that at any given value of Ro c , a different frequency ration exists. Then, using Fig. 2, a unique St c number corresponding to the combined Roshko number (Ro c ), can be derived. Thus, for a given volumetric flow rate, the combined frequency (fj + f 2 ) remains constant as the viscosity changes, but the frequency ratio (f 2 /fi) will vary.
• differential pressures there are a number of meters which use differential pressures, including, but not limited to, measuring the differential pressure across an orifice, across a blunt body, across a rotor, with a pitot tube or using a wall static method.
• a target meter could similarly be used.
• measuring flow rates with a target meter, or by using an orifice, or across a blunt body and across rotors are all sensitive to Reynolds numbers and fluid density. Since the kinematic viscosity is assumed to be unknown (although it can be mathematically determined) in the dual rotor meter discussed previously, using such methods essentially defeats the purpose of same, namely, the eliinination of viscosity as a variable.
• Fig. 10 shows a dual rotor meter 10 with a pitot tube 12 and wall static 14 installed.
• pitot tube 12 is used to calculate the velocity of the fluid as:
• V [(Pt - Ps)/p 2 where:
• N fluid velocity at the point of Pt measurement
• Pt total pressure
• Ps wall static pressure
• the density will change with temperature, but the differential pressure will change proportionally.
• the operating density is deterrnined independently of other variables.
• the dual rotor turbine meter has deterrnined the volumetric flow rate and the pitot tube/wall static have isolated the density, both independently of secondary variables.
• the average velocity in the duct is computed as:
• the velocity measured by the pitot tube is local or point velocity while the velocity computed from the flow rate is an average velocity.
• the proportionality constant K may actually vary somewhat with N avg or q but is easily
• One of the major advantages for use of a dual rotor turbine meter is the wide operating range, or turndown, of such meters.
• one of the major disadvantages of the pitot tube/wall static port is the small operating range of same.
• the velocity measured in a pitot tube is a function of the square root of the differential pressure and density.
• pressure transducers are normally rated as a percentage of full scale, a 16:1 ratio is generally all that can be tolerated. Note that there are methods to extend this limit, such as stacked differential pressure devices, or simply accepting a reduced accuracy in an extended range.
• another solution is also possible with particular application to hydrocarbon fluids such as jet fuel.
• the density versus temperature curve for most hydrocarbon fluids changes significantly from one batch to another.
• the batch of fluid on which the meter is employed is changed periodically.
• the change in density is a simple function of temperature (and pressure to a lesser degree in high pressure applications).
• the density measurement may be extrapolated from previously obtained data.
• the density data for a particular batch of fluid is maintained and accumulates, subject to data storage limitations, until a new batch arrives. Once a new batch arrives, the data is purged and new data added to allow for accurate extrapolation outside the operating range of the pitot tube. Until enough data is accumulated to make an accurate extrapolation, textbook averages can be used as temperature/density measurements.
• Fig. 8 show the typical accumulation of density data during the operation of the system.
• a running average, standard deviation computation or other form of limiting the very large number of data points may be used if needed to keep the data from oveiwhelming the processor.
• the current operating temperature is actually used to determine the density from the defined curve.
• the measured density points are used only to continually define the temperature versus density curve.

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• Physics & Mathematics (AREA)
• Fluid Mechanics (AREA)
• General Physics & Mathematics (AREA)
• Measuring Volume Flow (AREA)

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• 2002
  • 2002-02-07 US US10/071,636 patent/US6692535B2/en not_active Expired - Lifetime
• 2003
  • 2003-02-07 WO PCT/US2003/003524 patent/WO2003067199A2/en active Application Filing
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